AIRPLANE
FLIGHT
SUPPLEMENT 4
PRIMUS EPIC - FLIGHT
MANAGEMENT SYSTEM
ANAC APPROVED S4-10
REVISION 15 code 01 Page 11
Copyright © by Embraer. Refer to cover page for details.
ENGINE FAILURE
For airplanes with VNAV enabled:
Engine Failure Procedure........................................ ACCOMPLISH
Speed Selector Knob............................................... MAN
Altitude..................................................................... SET
FMS Cruise Altitude................................................. AS REQUIRED
FMS FAILURE
An FMS failure is indicated by the loss of all data on the PFD and MFD
maps. All data will be blanked, or dashed. A large “X” is displayed in
place of the lateral deviation indicator. An “FMS1 FAIL” or “FMS2 FAIL”
CAS message will also be displayed.
If an FMS failure occurs, the offside FMS should be selected. If the
offside FMS is not available, the following procedures should be
followed, based on the nature of the operation:
FMS Failure Procedures (Off-side FMS not Available)
Operation Required Action
Non-RNP Terminal or En-route Use alternate source (VOR, NDB,
DME).
B-RNAV, P-RNAV, or RNP
operations
Contact ATC and declare inability to
continue B-RNAV, P-RNAV, or RNP
operations.
Non-RNP (excluding GPS
required) Approach
Use alternate source, if available
(VOR, NDB). If not available, declare
missed approach.
RNP-0.3 or GPS required
approach
Declare Missed Approach.
Remote Operations Contact ATC and declare loss of
long range navigation capability.